EP3684481A1 - Shuttlecock - Google Patents

Shuttlecock

Info

Publication number
EP3684481A1
EP3684481A1 EP18895735.1A EP18895735A EP3684481A1 EP 3684481 A1 EP3684481 A1 EP 3684481A1 EP 18895735 A EP18895735 A EP 18895735A EP 3684481 A1 EP3684481 A1 EP 3684481A1
Authority
EP
European Patent Office
Prior art keywords
shuttlecock
segments
lower lip
recessed
tip
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP18895735.1A
Other languages
German (de)
French (fr)
Other versions
EP3684481C0 (en
EP3684481B1 (en
EP3684481A4 (en
Inventor
Anthony Bert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Badminton World Federation
Original Assignee
Badminton World Federation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Badminton World Federation filed Critical Badminton World Federation
Publication of EP3684481A1 publication Critical patent/EP3684481A1/en
Publication of EP3684481A4 publication Critical patent/EP3684481A4/en
Application granted granted Critical
Publication of EP3684481C0 publication Critical patent/EP3684481C0/en
Publication of EP3684481B1 publication Critical patent/EP3684481B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B67/00—Sporting games or accessories therefor, not provided for in groups A63B1/00 - A63B65/00
    • A63B67/18—Badminton or similar games with feathered missiles
    • A63B67/183—Feathered missiles
    • A63B67/187—Shuttlecocks
    • A63B67/193—Shuttlecocks with all feathers made in one piece
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B67/00—Sporting games or accessories therefor, not provided for in groups A63B1/00 - A63B65/00
    • A63B67/18—Badminton or similar games with feathered missiles
    • A63B67/183—Feathered missiles
    • A63B67/187—Shuttlecocks
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B2102/00—Application of clubs, bats, rackets or the like to the sporting activity ; particular sports involving the use of balls and clubs, bats, rackets, or the like
    • A63B2102/04—Badminton
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B2209/00—Characteristics of used materials
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B2225/00—Miscellaneous features of sport apparatus, devices or equipment
    • A63B2225/01—Special aerodynamic features, e.g. airfoil shapes, wings or air passages

Definitions

  • the invention relates to a shuttlecock, particularly a badminton shuttlecock with reduced side wind interference and enhanced longitudinal angular stability.
  • a conventional or an existing shuttlecock is typically having narrower space between each stem and shuttlecock with such design is generally sensitive to external disturbance of the surrounding area, particularly varying wind strength which could eventually influence the flight performance of the shuttlecock in a badminton game or activity. This external disturbance could be limited or reduced when the badminton game or activity is played in an indoor badminton court.
  • the presence of wind condition of random magnitude and direction could greatly deteriorate the flight performance of the shuttlecock as a result of strong cross wind interference since air flow is restricted due to the narrower space between each stem.
  • the present invention presents a shuttlecock with larger space between each stem as compared to that of the conventional or an existing shuttlecock by which such design enables the shuttlecock to possess increased resistance to flight deviation caused by challenging wind conditions and thus enhancing the flight stability of the shuttlecock, either in indoor or outdoor conditions.
  • the present invention relates to a shuttlecock that is configured to reduce side wind interference and enhance the longitudinal angular stability.
  • the shuttlecock comprises a tip and a plurality of segments extending away from the tip.
  • the tip comprises a recessed upper lip, a base and a recessed lower lip.
  • the base is formed between the recessed upper lip and the recessed lower lip.
  • the tip of the shuttlecock is preferably engaged to the plurality of segments by snap and fit mechanism.
  • the snap and fit mechanism is an assembly technique that interlocks two flexible parts into an integral component without using any adhesive agent or fastener. It will be appreciated that by using snap and fit mechanism, the material could be reduced.
  • the plurality of segments is extending from the recessed lower lip, integrally formed and arranged in an annular array.
  • each of the plurality of segments is having a pair of spaced apart, diverging stems with a blade provided between the stems.
  • the blade of the segment is positioned at the end of the segment distal from the recessed lower lip.
  • the blade of the segment is provided with a plurality of perforations thereon.
  • a sizable central opening is formed at the centre portion of each of the plurality of segments.
  • the central opening of the segment is configured to allow passage of cross wind so as to reduce cross wind interference.
  • the central opening of the segment could reduce the mass of the segment beyond the lower lip which resulted in the centre of gravity of the shuttlecock being moved closer to the tip.
  • the tip of the shuttlecock is provided with a cork.
  • the cork is preferably having a hemispherical dome and a cylindrical base. If desired, the surface of the hemispherical dome of the cork can be provided with a plurality of dimples so as to enhance the aesthetic appearance of the shuttlecock.
  • the shuttlecock may be formed from polyamide (preferably nylon), polyethylene, polyester, polypropylene, polystyrene, polytetrafluoroethylene, polyurethane, polyvinylchloride or any other materials deemed suitable.
  • Fig. 1 shows a shuttlecock without any cork.
  • Fig. 2 shows a shuttlecock provided with a cork.
  • the present invention relates to a shuttlecock and more particularly a shuttlecock with reduced side wind interference and enhanced longitudinal angular stability.
  • this specification will describe the present invention according to the preferred embodiments of the present invention.
  • limiting the description to the preferred embodiments of the invention is merely to facilitate discussion of the present invention and it is envisioned that those skilled in the art may devise various modifications and equivalents without departing from the scope of the appended claims.
  • the shuttlecock according to the preferred mode of carrying out the present invention will now be described in accordance to the accompanying drawings Figs. 1 and 2, either individually or combination thereof.
  • the shuttlecock (1) comprises a tip (9) and a plurality of segments (29).
  • the tip (9) and the segments (29) are connected by snap and fit mechanism.
  • the snap and fit mechanism is an assembly technique that interlocks two flexible parts into an integral component without using any adhesive agent or fastener and it will be appreciated that this assembly technique could save the material cost for the production of the shuttlecock (1).
  • the tip (9) of the shuttlecock (1) is having a recessed upper lip (3), a base (5) and a recessed lower lip (7). It should be noted that the base (5) of the tip (9) is formed between the recessed upper lip (3) and the recessed lower lip (7).
  • the plurality of segments (29) are extending away from the recessed lower lip (7) of the tip (9), integrally formed and arranged in an annular array.
  • a sizable central opening (13) is formed at the centre portion of each of the plurality of segments (29).
  • the central opening (13) of the segment (29) is configured to allow passage of cross wind to reduce cross wind interference.
  • the central opening (13) of the segment (29) could reduce the mass of the segments (29) beyond the lower lip (7) which resulted in the centre of gravity of the shuttlecock (1) being moved closer to the tip (9).
  • the nearer the centre of gravity towards the tip (9) of the shuttlecock (1) the higher the longitudinal angular stability of the shuttlecock (1), thus reducing wobbling during the turnover phase of the shuttlecock (1).
  • the central opening (13) of the segment (29) may be in the form of rectangular, hexagonal or triangular shape.
  • each of the plurality of segments (29) has a pair of spaced apart, diverging stems (11).
  • the length of each stem (11) may range from lOmm to 50mm and the angle between the stem (11) and the tip (9) of the shuttlecock (1) may range from 90 degrees to 120 degrees.
  • the stems (1 1) may be in the form of any other appropriate profiles including but not limited to a circular section, tubular section, L section, X section or rectangular section.
  • a blade (15) is provided between the stems (11) as illustrated in Fig. 1.
  • the blade (15) of the segment (29) is preferably positioned at the end of the segment (29) distal from the recessed lower lip (7) and provided with a plurality of perforations (17) thereon.
  • the plurality of perforations (17) of the blade (15) may be in the form of circular, triangular or square shape in any desired sizes.
  • the plurality of perforations (17) of the blade (15) is configured to create desired air permeability to allow air to flow through and over the blades (15) of the segments (29) so as to result an axial spin of the shuttlecock (1).
  • the axial spin assists in stabilising the trajectory profile of the shuttlecock (1).
  • the blade (15) of the segment (29) is having a parabolic curved shape. It will be appreciated that such configuration could further reduce the cross wind interference.
  • the plurality of blades (15) of the segments (29) collectively formed a skirt (19) of the shuttlecock (1).
  • the skirt (19) preferably has a diameter of 67mm at an opening (31) and a height of 20mm.
  • the height of the skirt (19) provides reduced side profile while retaining the required pitching moment for angular stability in the longitudinal directions.
  • the diameter of the skirt (19) at the opening (31) may range from 55mm to 80mm. It will be appreciated that by increasing the diameter of the skirt, the drag experienced by the shuttlecock could also be increased.
  • the height of the skirt (19) is preferably range from 5mm to 25mm. It should be noted that by increasing the height of the skirt, the angular stability of the shuttlecock could be increased at the expense of reduced resistance to side wind interference.
  • the shuttlecock (1) of the present invention is also provided with a cork (5) as illustrated in Fig. 2.
  • the cork is having a hemispherical dome and a cylindrical base and is suitably engaged with the tip (9) of the shuttlecock by snap and fit mechanism.
  • the surface of the hemispherical dome of the cork is provided with a plurality of dimples (31) so as to enhance the aesthetic appearance of the shuttlecock (1).
  • the shuttlecock (1) of the present invention may be formed from polyamide (preferably nylon), polyethylene, polyester, polypropylene, polystyrene, polytetrafluoroethylene, polyurethane, polyvinylchloride or any other materials deemed suitable.

Landscapes

  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Physical Education & Sports Medicine (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)

Abstract

The invention relates to a shuttlecock (1). The shuttlecock (1) comprises a tip (9) having a recessed upper lip (3), a recessed lower lip (7) and a base (5) formed between the recessed upper lip (3) and the recessed lower lip (7). The shuttlecock (1) has a plurality of segments (29) extending away from the recessed lower lip (7), integrally formed and arranged in an annular array. Each of the plurality of segments (29) has a pair of spaced apart, diverging stems (11) with a blade (15) provided between the stems (11) at the end of the segment (29) distal from the recessed lower lip (7). The blade (15) comprises a plurality of perforations (17) thereon. There is a sizable central opening (13) formed at the centre portion of each of the plurality of segments (29) wherein the central opening (13) of the segment (29) is configured to allow passage of cross wind to reduce cross wind interference and the reduced mass of the segments (29) beyond the lower lip (7) resulting in the centre of gravity of the shuttlecock (1) being moved closer to the tip (9).

Description

SHUTTLECOCK
FIELD OF INVENTION
The invention relates to a shuttlecock, particularly a badminton shuttlecock with reduced side wind interference and enhanced longitudinal angular stability.
BACKGROUND OF THE INVENTION
A conventional or an existing shuttlecock is typically having narrower space between each stem and shuttlecock with such design is generally sensitive to external disturbance of the surrounding area, particularly varying wind strength which could eventually influence the flight performance of the shuttlecock in a badminton game or activity. This external disturbance could be limited or reduced when the badminton game or activity is played in an indoor badminton court. However, at the outdoor environment, the presence of wind condition of random magnitude and direction could greatly deteriorate the flight performance of the shuttlecock as a result of strong cross wind interference since air flow is restricted due to the narrower space between each stem.
To overcome the aforementioned deficiencies, the present invention presents a shuttlecock with larger space between each stem as compared to that of the conventional or an existing shuttlecock by which such design enables the shuttlecock to possess increased resistance to flight deviation caused by challenging wind conditions and thus enhancing the flight stability of the shuttlecock, either in indoor or outdoor conditions. SUMMARY OF THE INVENTION
The present invention relates to a shuttlecock that is configured to reduce side wind interference and enhance the longitudinal angular stability.
According to the present invention, the shuttlecock comprises a tip and a plurality of segments extending away from the tip. In the preferred embodiment, the tip comprises a recessed upper lip, a base and a recessed lower lip. The base is formed between the recessed upper lip and the recessed lower lip. The tip of the shuttlecock is preferably engaged to the plurality of segments by snap and fit mechanism. The snap and fit mechanism is an assembly technique that interlocks two flexible parts into an integral component without using any adhesive agent or fastener. It will be appreciated that by using snap and fit mechanism, the material could be reduced.
Preferably, the plurality of segments is extending from the recessed lower lip, integrally formed and arranged in an annular array. In the preferred embodiment of the present invention, each of the plurality of segments is having a pair of spaced apart, diverging stems with a blade provided between the stems. It should be noted the blade of the segment is positioned at the end of the segment distal from the recessed lower lip. Preferably, the blade of the segment is provided with a plurality of perforations thereon.
According to the preferred embodiment of the present invention, a sizable central opening is formed at the centre portion of each of the plurality of segments. It will be appreciated that the central opening of the segment is configured to allow passage of cross wind so as to reduce cross wind interference. It should be noted that the central opening of the segment could reduce the mass of the segment beyond the lower lip which resulted in the centre of gravity of the shuttlecock being moved closer to the tip. In the preferred embodiment, the tip of the shuttlecock is provided with a cork. The cork is preferably having a hemispherical dome and a cylindrical base. If desired, the surface of the hemispherical dome of the cork can be provided with a plurality of dimples so as to enhance the aesthetic appearance of the shuttlecock.
By way of example but not limitation, the shuttlecock may be formed from polyamide (preferably nylon), polyethylene, polyester, polypropylene, polystyrene, polytetrafluoroethylene, polyurethane, polyvinylchloride or any other materials deemed suitable.
The apparatus of the present invention consists of several novel features and a combination of parts hereinafter fully described and illustrated in the accompanying descriptions and drawings, it being understood that various changes in the details may be made without departing from the scope of the invention or sacrificing any of the advantages of the present invention.
BRIEF DESCRIPTION OF THE DRAWINGS
The present invention will be fully understood from the detailed descriptions given herein below and the accompanying drawings which are given by way of illustration only, and thus are not limitative of the present invention, wherein:
Fig. 1 shows a shuttlecock without any cork.
Fig. 2 shows a shuttlecock provided with a cork.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
The present invention relates to a shuttlecock and more particularly a shuttlecock with reduced side wind interference and enhanced longitudinal angular stability. Hereinafter, this specification will describe the present invention according to the preferred embodiments of the present invention. However, it is to be understood that limiting the description to the preferred embodiments of the invention is merely to facilitate discussion of the present invention and it is envisioned that those skilled in the art may devise various modifications and equivalents without departing from the scope of the appended claims. The shuttlecock according to the preferred mode of carrying out the present invention will now be described in accordance to the accompanying drawings Figs. 1 and 2, either individually or combination thereof.
Referring to Fig. 1, illustrated therein is a shuttlecock (1) of the preferred embodiment of the present invention. The shuttlecock (1) comprises a tip (9) and a plurality of segments (29). Preferably, the tip (9) and the segments (29) are connected by snap and fit mechanism.
The snap and fit mechanism is an assembly technique that interlocks two flexible parts into an integral component without using any adhesive agent or fastener and it will be appreciated that this assembly technique could save the material cost for the production of the shuttlecock (1). In the preferred embodiment, the tip (9) of the shuttlecock (1) is having a recessed upper lip (3), a base (5) and a recessed lower lip (7). It should be noted that the base (5) of the tip (9) is formed between the recessed upper lip (3) and the recessed lower lip (7). According to the preferred embodiment of the present invention, the plurality of segments (29) are extending away from the recessed lower lip (7) of the tip (9), integrally formed and arranged in an annular array.
In the preferred embodiment of the present invention, a sizable central opening (13) is formed at the centre portion of each of the plurality of segments (29). It should be noted that the central opening (13) of the segment (29) is configured to allow passage of cross wind to reduce cross wind interference. It will be appreciated that the central opening (13) of the segment (29) could reduce the mass of the segments (29) beyond the lower lip (7) which resulted in the centre of gravity of the shuttlecock (1) being moved closer to the tip (9). It should be noted that the nearer the centre of gravity towards the tip (9) of the shuttlecock (1), the higher the longitudinal angular stability of the shuttlecock (1), thus reducing wobbling during the turnover phase of the shuttlecock (1). By way of example but not limitation, the central opening (13) of the segment (29) may be in the form of rectangular, hexagonal or triangular shape.
In the preferred embodiment of the present invention, each of the plurality of segments (29) has a pair of spaced apart, diverging stems (11). Preferably, the length of each stem (11) may range from lOmm to 50mm and the angle between the stem (11) and the tip (9) of the shuttlecock (1) may range from 90 degrees to 120 degrees. It should be noted that the stems (1 1) may be in the form of any other appropriate profiles including but not limited to a circular section, tubular section, L section, X section or rectangular section.
In the preferred embodiment, a blade (15) is provided between the stems (11) as illustrated in Fig. 1. The blade (15) of the segment (29) is preferably positioned at the end of the segment (29) distal from the recessed lower lip (7) and provided with a plurality of perforations (17) thereon. By way of example but not limitation, the plurality of perforations (17) of the blade (15) may be in the form of circular, triangular or square shape in any desired sizes. The plurality of perforations (17) of the blade (15) is configured to create desired air permeability to allow air to flow through and over the blades (15) of the segments (29) so as to result an axial spin of the shuttlecock (1). The axial spin assists in stabilising the trajectory profile of the shuttlecock (1). Preferably, the blade (15) of the segment (29) is having a parabolic curved shape. It will be appreciated that such configuration could further reduce the cross wind interference.
According to the preferred embodiment of the present invention, the plurality of blades (15) of the segments (29) collectively formed a skirt (19) of the shuttlecock (1). The skirt (19) preferably has a diameter of 67mm at an opening (31) and a height of 20mm. The height of the skirt (19) provides reduced side profile while retaining the required pitching moment for angular stability in the longitudinal directions. Optionally, the diameter of the skirt (19) at the opening (31) may range from 55mm to 80mm. It will be appreciated that by increasing the diameter of the skirt, the drag experienced by the shuttlecock could also be increased. The height of the skirt (19) is preferably range from 5mm to 25mm. It should be noted that by increasing the height of the skirt, the angular stability of the shuttlecock could be increased at the expense of reduced resistance to side wind interference.
The shuttlecock (1) of the present invention is also provided with a cork (5) as illustrated in Fig. 2. Preferably, the cork is having a hemispherical dome and a cylindrical base and is suitably engaged with the tip (9) of the shuttlecock by snap and fit mechanism. If desired, the surface of the hemispherical dome of the cork is provided with a plurality of dimples (31) so as to enhance the aesthetic appearance of the shuttlecock (1).
By way of example but not limitation, the shuttlecock (1) of the present invention may be formed from polyamide (preferably nylon), polyethylene, polyester, polypropylene, polystyrene, polytetrafluoroethylene, polyurethane, polyvinylchloride or any other materials deemed suitable.
The foregoing description is considered as illustration of the principles of the invention. Furthermore, since numerous modifications and changes will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation shown and described, and accordingly all suitable modifications and equivalents may be resorted to, falling within the scope of the invention.

Claims

1 A shuttlecock (1) comprising: a tip (9) having a recessed upper lip (3), a recessed lower lip (7) and a base (5) formed between the recessed upper lip (3) and the recessed lower lip (7); and a plurality of segments (29) extending away from the recessed lower lip (7), each of the plurality of segments (29) has a pair of spaced apart, diverging stems (11) with a blade (15) provided between the stems (11) at the end of the segment (29) distal from the recessed lower lip (7), the blade (15) has a plurality of perforations (17) thereon and the plurality of segments (29) are integrally formed and arranged in an annular array; characterised in that: there is a sizable central opening (13) at the centre portion of each of the plurality of segments (29) wherein the central opening (13) of the segment (29) is configured to allow passage of cross wind to reduce cross wind interference and the reduced mass of the segments (29) beyond the lower lip (7) resulted in the centre of gravity of the shuttlecock (1) being moved closer to the tip (9).
2. The shuttlecock (1) according to Claim 1, wherein the stems (11) may be in the form of circular, tubular, L, X, rectangular or triangular shape.
3. The shuttlecock (1) according to Claim 1, wherein the central opening (13) of the segment (29) may be in the form of rectangular, hexagonal or triangular shape.
4. The shuttlecock (1) according to Claim 1, wherein the plurality of perforations (17) of the blade (15) may be in the form of circular, triangular or square shape.
5. The shuttlecock (1) according to Claim 1, wherein the shuttlecock (1) is provided with a cork (5) suitably engaged with the tip (9) by snap and fit mechanism.
6. The shuttlecock (1) according to Claim 1, wherein the blade (15) of the plurality of segments (29) collectively forms a skirt (19).
EP18895735.1A 2017-12-15 2018-12-07 Shuttlecock Active EP3684481B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
MYPI2017001865A MY188783A (en) 2017-12-15 2017-12-15 Shuttlecock
PCT/MY2018/050089 WO2019132649A1 (en) 2017-12-15 2018-12-07 Shuttlecock

Publications (4)

Publication Number Publication Date
EP3684481A1 true EP3684481A1 (en) 2020-07-29
EP3684481A4 EP3684481A4 (en) 2021-06-09
EP3684481C0 EP3684481C0 (en) 2024-02-21
EP3684481B1 EP3684481B1 (en) 2024-02-21

Family

ID=67064030

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18895735.1A Active EP3684481B1 (en) 2017-12-15 2018-12-07 Shuttlecock

Country Status (7)

Country Link
EP (1) EP3684481B1 (en)
JP (1) JP7069310B2 (en)
KR (1) KR102473635B1 (en)
CN (1) CN111212681B (en)
MY (1) MY188783A (en)
TW (1) TWI705842B (en)
WO (1) WO2019132649A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111870910A (en) * 2020-08-04 2020-11-03 安徽三才体育用品有限公司 Outdoor ball
CN111870913A (en) * 2020-08-04 2020-11-03 安徽三才体育用品有限公司 Splicing three-section outdoor ball
CN111870911A (en) * 2020-08-04 2020-11-03 安徽三才体育用品有限公司 Outdoor ball and racket
CN111870912A (en) * 2020-08-04 2020-11-03 安徽三才体育用品有限公司 Butt-joint three-section outdoor ball
US20230201683A1 (en) * 2021-12-23 2023-06-29 Mario Caya Golf tee and golf tee kit

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4318029Y1 (en) * 1965-07-19 1968-07-25
GB1103364A (en) * 1966-10-04 1968-02-14 Carlton Tyre Saving Co Ltd Improvements in or relating to shuttlecocks
GB1386697A (en) * 1972-04-29 1975-03-12 Dunlop Ltd Shuttlecocks
US3904205A (en) * 1972-06-16 1975-09-09 Maurice Robinson Shuttlecock
GB2059271B (en) * 1979-04-06 1982-12-15 Reinforced Shuttlecocks Ltd Shuttlecocks
ZA802606B (en) * 1979-05-10 1981-08-26 Dunlop Ltd Shuttlecocks
JPS6019745Y2 (en) * 1982-03-12 1985-06-13 株式会社ゴ−セン Synthetic resin badminton shuttlecock
GB2279580A (en) * 1993-07-10 1995-01-11 Peter Shu Chun Cheng Shuttlecock
US6682448B2 (en) * 1999-03-18 2004-01-27 Bradford C. Jamison Play device
JP2007521083A (en) 2003-07-07 2007-08-02 ダイ−イル キム Shuttlecock
JP2006081713A (en) 2004-09-16 2006-03-30 Koji Okai Shuttlecock for batting practice
TWM292580U (en) * 2005-12-30 2006-06-21 Danfany Purification Technolog Water conditioner for water purification equipment
DE102007041169B8 (en) * 2007-08-24 2014-09-04 Speedminton Gmbh Shuttlecock
JP5525686B2 (en) 2007-11-26 2014-06-18 ヨネックス株式会社 shuttle
CN101977659B (en) 2007-11-30 2012-07-04 尤尼克斯株式会社 Shuttlecock
CN201404647Y (en) * 2009-05-22 2010-02-17 罗兵 Wind resistance badminton
KR200447562Y1 (en) 2009-07-18 2010-02-03 김상웅 Racket game shuttlecock for narrow space
CN201832386U (en) * 2010-03-16 2011-05-18 张文广 Shuttlecock
KR101553829B1 (en) * 2013-12-30 2015-09-18 허봉락 Korean shuttlecock ball for kicking
US9132328B1 (en) * 2014-07-18 2015-09-15 Long Daole Shuttlecock type game device
CN204864826U (en) * 2015-06-18 2015-12-16 盛宇杰 Quick badminton

Also Published As

Publication number Publication date
CN111212681A (en) 2020-05-29
JP7069310B2 (en) 2022-05-17
EP3684481C0 (en) 2024-02-21
KR20200099142A (en) 2020-08-21
EP3684481B1 (en) 2024-02-21
TW201927380A (en) 2019-07-16
EP3684481A4 (en) 2021-06-09
TWI705842B (en) 2020-10-01
CN111212681B (en) 2021-09-21
MY188783A (en) 2021-12-30
KR102473635B1 (en) 2022-12-02
WO2019132649A1 (en) 2019-07-04
JP2021508260A (en) 2021-03-04

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